N443LX

Cancelled 2024

Deregistered aircraft · 1999 Raytheon 400A · Pratt & Whitney Canada JT15D 5 series

Cancelled
March 14, 2024
Status when cancelled
Valid registration
Serial number
RK-237
Year built
1999
Type
Fixed wing multi engine
Engine
Turbo-fan
Airworthiness
Standard, transport
Airworthiness date
May 29, 1999
Certificate issued
December 30, 2009
Last registry action
July 18, 2023
Mode S code
A556D2
Owner when cancelled
Flight Options LLC
Owner type
LLC

From the FAA registry file of November 4, 2026, cancelled registrations. Owners’ street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

Service difficulty reports · 15

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR DJFA20120827001Mount · crackedDURING INSPECTION OF NR 1 ENGINE FORWARD MOUNT AFT BRACKET AS CALLED OUT BY AD 2002-01-23, THE MOUNT WAS FOUND CRACKED. MX R & R BRACKET WITH KIT 128-4035, REV B.Aug 27, 2012 · N443LX · Beech 400A · Engine Mount SectionSDR DJFA20120508002Rib · crackedDURING SCHDULED INSPECTION, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPMay 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508003Rib · crackedDURING SCHDULED INSP, MX TECH FOUND 8 RIBS CRACKED IN THE HORIZ STAB. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACED IMay 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508004Rib · crackedDURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACED May 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508005Rib · crackedDURING SCHDULED INSP, MX TECH FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REMay 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508006Rib · crackedDURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACED May 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508007Rib · crackedDURING SCHDULED INSP, MX TX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EA CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACMay 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508008Rib · crackedDURING SCHDULED INSP, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE REPLACEMay 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA20120508001Rib · crackedDURING SCHDULED INSPECTION, MX FOUND 8 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 8 RIBS WERE RMay 8, 2012 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/RibSDR DJFA2011012Valve · inoperativeDURING TAXI, AFTER LANDING, CREW NOTED LOSS OF BRAKING ACTION FROM THE PILOTS AND COPILOTS RT BRAKE PEDAL. BRAKING ACTION WAS RETURNED AFTER REPEATED PUMPING OF THE PEDAL. MX FOUND POWER BRAKE ANTI-SKID CONTROL VALVE FAILED. THE UNIT WAS REPLACED.Mar 30, 2011 · N443LX · Beech 400A · Landing Gear Brake SystemSDR DJFA2011009Power Supply · failedDURING FLIGHT, CREW REPORTED SMOKE AND FUMES IN THE COCKPIT. ACFT DIVERTED AND, AFTER LANDING, CREW REPORTED SMOKE DISSIPATED WHEN CTR PEDESTAL LIGHTS WERE EXTINGUISHED. MAINTENANCE FOUND THE INSTRUMENT PANEL DIMMER OUTPUT INCORRECT AND THE ALTITUDE AWARENEFeb 8, 2011 · N443LX · Beech 400A · Instrument PanelSDR DJFA2010036Power Supply · failedACFT DIVERTED, DUE TO SMOKE SMELL IN COCKPIT. EMERGENCY WAS DECLARED. MX EVALUATED AND CONFIRMED "BURNED ELECTRICAL" ODOR FROM ALTITUDE AWARENESS PANEL. ALSO FOUND INSTRUMENT LIGHT POWER SUPPLY OUTPUT AT 118VAC. R & R THE INSTRUMENT LIGHT POWER SUPPLY AND Nov 27, 2010 · N443LX · Beech 400A · Instrument System WiringSDR DJFA2009031Brake Assy · weakON LANDING CREW REPORTED INITIAL ATTEMPTS TO BRAKE WERE UNSUCCESSFUL. CREW HAD TO PUMP THE BRAKES IN ORDER TO OBTAIN BRAKING ACTION. MAINTENANCE FOUND THE BRAKE SYSTEM NEEDED TO BE BLED.Jul 29, 2009 · N443LX · Beech 400A · Landing Gear Brake SystemSDR DJFA2009015Brake Sys · malfunctionedON LANDING, THE FLIGHT CREW REPORTED ABNORMAL PRESSURE REQUIRED TO STOP THE ACFT. SUCH ABNORMAL BRAKING ACTION CAUSED THE RT BRAKE TO GRAB. ACFT FINALLY CAME TO A STOP SAFELY. MX BLED THE BRAKE SYS AND FOUND AIR IN THE RT BRAKE LINE. THE SYS WAS RESTORED TOApr 19, 2009 · N443LX · Beech 400A · Landing Gear Brake SystemSDR DJFA2008012Rib · crackedDURING A SCHEDULED MAINT VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSP OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB RIB WAS FOUND CRACKED. DETAILED INSP INSTRUCTIONS OF THIS AREA ARE OUTLINED IN COMMUNIQUE' NR 70. OPENJan 29, 2008 · N443LX · Beech 400A · Horizontal Stabilizer, Spar/Rib